GB2134059B - Composite helicopter fuselage - Google Patents

Composite helicopter fuselage

Info

Publication number
GB2134059B
GB2134059B GB08400187A GB8400187A GB2134059B GB 2134059 B GB2134059 B GB 2134059B GB 08400187 A GB08400187 A GB 08400187A GB 8400187 A GB8400187 A GB 8400187A GB 2134059 B GB2134059 B GB 2134059B
Authority
GB
United Kingdom
Prior art keywords
helicopter fuselage
composite helicopter
composite
fuselage
helicopter
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB08400187A
Other versions
GB2134059A (en
GB8400187D0 (en
Inventor
Reginald Ernest Swinfield
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Westland Group PLC
Original Assignee
Westland PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westland PLC filed Critical Westland PLC
Priority to GB08400187A priority Critical patent/GB2134059B/en
Publication of GB8400187D0 publication Critical patent/GB8400187D0/en
Publication of GB2134059A publication Critical patent/GB2134059A/en
Application granted granted Critical
Publication of GB2134059B publication Critical patent/GB2134059B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
GB08400187A 1983-01-25 1984-01-05 Composite helicopter fuselage Expired GB2134059B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08400187A GB2134059B (en) 1983-01-25 1984-01-05 Composite helicopter fuselage

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8301991 1983-01-25
GB08400187A GB2134059B (en) 1983-01-25 1984-01-05 Composite helicopter fuselage

Publications (3)

Publication Number Publication Date
GB8400187D0 GB8400187D0 (en) 1984-02-08
GB2134059A GB2134059A (en) 1984-08-08
GB2134059B true GB2134059B (en) 1986-06-25

Family

ID=26285016

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08400187A Expired GB2134059B (en) 1983-01-25 1984-01-05 Composite helicopter fuselage

Country Status (1)

Country Link
GB (1) GB2134059B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2632604B1 (en) * 1988-06-08 1991-07-12 Aerospatiale FRAME OF COMPOSITE MATERIAL IN PARTICULAR FOR AIRCRAFT FUSELAGE, AND METHOD FOR MANUFACTURING SAME
DE19639339B4 (en) * 1996-09-25 2004-06-24 Dwa Deutsche Waggonbau Gmbh Shell structure made of fiber-reinforced plastic for vehicles or containers, in particular for car bodies of rail vehicles
JP3997047B2 (en) * 2000-05-01 2007-10-24 本田技研工業株式会社 Bonding structure of skin and pressure bulkhead
US8920594B2 (en) 2005-08-03 2014-12-30 Sikorsky Aircraft Corporation Composite thermoplastic matrix airframe structure and method of manufacture therefore
DE102006002248B4 (en) * 2006-01-17 2008-01-03 Airbus Deutschland Gmbh Structural construction for a fuselage
FR2921899B1 (en) * 2007-10-04 2011-04-15 Airbus France METHOD FOR LOCALLY REINFORCING COMPOSITE MATERIAL ELEMENT AND CENTRAL BOAT BOILER FOR REINFORCED AIRCRAFT
ES2383986B1 (en) * 2009-12-30 2013-05-16 Airbus Operations, S.L. AIRCRAFT FUSELAGE NOTEBOOK IN COMPOSITE MATERIAL WITH STABILIZED SOUL.
US8317135B2 (en) * 2010-04-19 2012-11-27 Sabreliner Corporation Flexible mounting assembly for an air frame structure
US20180327071A1 (en) * 2017-05-10 2018-11-15 The Boeing Company Systems and methods for aircraft integrated composite frames

Also Published As

Publication number Publication date
GB2134059A (en) 1984-08-08
GB8400187D0 (en) 1984-02-08

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee